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normally occurs on the first start of the day.
19. Single Rudder Limit Message.........................................................................ON
Right engine only running.
20. Hydraulic Pressure ..............................................................................CHECKED
21. Flight Data Recorder Fail Message................................................CHECK OUT
22. Second Engine Start ....................................REPEAT STEPS 10 THROUGH 18
23. Single Rudder Limit Message.......................................................................OUT
24. Hydraulic Pressure ..............................................................................CHECKED
OPERATING MANUAL
EXPANDED NORMAL PROCEDURES 03-03-00
Page 7
May 30/02
Revision 7
OPERATING MANUAL
THIS PAGE IS INTENTIONALLY LEFT BLANK.
03-03-00 EXPANDED NORMAL PROCEDURES
Page 8
May 30/02
BEFORE TAKEOFF PROCEDURES
03-04-10: After Starting Engines
1. Start Master.....................................................................................................OFF
2. Electrical Power................................................................................................ON
3. External Electrical Power / Air ...................................OFF / CARTS REMOVED
4. Auxiliary Electrical Power / Air / Engine Bleed Air......................AS DESIRED
NOTE:
Only one source of bleed air, either APU or engines,
should be selected after engines are started. This is to
prevent thermal transients on the APU or possible
damage to the APU when the power levers are moved
from idle. With the engines as the source of bleed air,
ensure the ISOLATION valve is CLOSED.
5. Battery Ammeters .....................................................................................CHECK
6. ESS DC Bus Power Source........................AUTO / LEFT MAIN ILLUMINATED
CAUTION
DO NOT DISPATCH WITH ESS DC BUS POWERED
BY BATTERIES.
7. Emergency Power .........................................................................................ARM
8. Doors ..........................................................................................................CLOSE
NOTE:
Check that the orange dot position indicator on each of
the six locking pins is visible.
9. Anti-Ice Heaters ................................................................................................ON
For airplanes SN 1096 and subsequent (5), and airplanes SN 1000 through 1095
(4).
10. Cowl / Wing Anti-Ice.....................................................CHECK / AS REQUIRED
NOTE:
Check or select cowl / wing anti-ice ON using engine
bleed air only to prevent excessive APU EGT.
11. Pressurization Control .....................................................AUTO / FLIGHT / SET
12. Fuel Boost Pumps / Crossflow Valve ..........................................ON / CLOSED
13. Nose Wheel Steering......................................................................................OFF
14. Ground Spoilers........................................................................................CHECK
NOTE:
Check on first flight of the day.
OPERATING MANUAL
EXPANDED NORMAL PROCEDURES 03-04-00
Page 1
May 30/02
Revision 7
15. Stall Barrier ...................................................................................................TEST
NOTE:
Check on first flight of the day. If flight time for the day
exceeds eight hours, a second stall barrier check is
required prior to the second flight of the day. See
Section 2A-27-20, Pitch Flight Control System.
16. Flight Controls / Rudder Torque Limiter ................................................CHECK
NOTE:
See Rudder Torque Limiter Check, Section 2A-27-30,
Yaw Flight Control System.
17. Yaw Damper......................................................................................................ON
18. Nose Wheel Steering .......................................................................................ON
19. Pedal Steering Disconnect Switch........................................ON / LIGHTS OUT
20. Auxiliary Hydraulic Pump........................................................................ARMED
21. Brake Test Switch (BITE) / Anti-Skid Test Switch....PRESS, THEN RELEASE
03-04-20: Taxi / Before Takeoff
1. Exterior Lights ..............................................................................AS REQUIRED
NOTE:
Limit ground operation of landing lights to five (5)
minutes.
2. Cowl / Wing Anti-Ice.....................................................................AS REQUIRED
NOTE:
Select cowl / wing anti-ice ON using engine bleed air
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湾流4操作手册 Gulfstream IV Operating Manual 3(33)
